Demonstrators for hybrid & innovative aeronautical propulsion systems
CONTEXT
Developing the low-carbon aircraft of tomorrow is a key concern for all aviation industry players and of major concern for achieving sustainability in the aviation sector.
Hybrid Electric propulsion is identified as a promising technology to reduce emissions, covering a wide range of aircraft.
This project aims to:
- Develop a predictive methodology for the dynamic calculation of hybrid shaft lines, validated on a partial bench,
- Develop and test a hybrid electric turboprop ground demonstrator.
FINANCING
